CN205554593U - A four shaft air vehicle for maritime search and rescue - Google Patents
A four shaft air vehicle for maritime search and rescue Download PDFInfo
- Publication number
- CN205554593U CN205554593U CN201620350718.8U CN201620350718U CN205554593U CN 205554593 U CN205554593 U CN 205554593U CN 201620350718 U CN201620350718 U CN 201620350718U CN 205554593 U CN205554593 U CN 205554593U
- Authority
- CN
- China
- Prior art keywords
- rescue
- chassis
- aircraft
- support bar
- maritime search
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Emergency Lowering Means (AREA)
Abstract
The utility model discloses a four shaft air vehicle for maritime search and rescue, including aircraft frame and chassis, aircraft rack surface four corners all is equipped with the screw base, the screw is connected at screw base top, aircraft frame bottom is equipped with the safety cover, the safety cover is connected to the chassis, the chassis surface is equipped with the back shaft, the back shaft top is equipped with data processor, the safety cover inner chamber is equipped with the searchlight, back shaft one side is equipped with camera device, the camera device surface is equipped with infrared probe, the chassis central point is equipped with the connecting axle, connecting axle one end is equipped with the support regulator, the support regulator rotates the joint support pole, the bracing piece end is equipped with spacing, the bracing piece with be equipped with the life buoy between spacing. This maritime life saving apparatus four shaft air vehicle, the function is various, and it makes a video recording to have takes photo by plane and the function of heat formation formation of image, can find the survivor fast, increases the efficiency of searching for aning rescue.
Description
Technical field
This utility model relates to space equipment technical field, a kind of aircraft for maritime search and rescue.
Background technology
Maritime search and rescue are always a global difficult problem, because the scope in sea is wide, situation on sea is changeful, when at sea accident occurs, often being difficult to the very first time looks for spot, traditional maritime search and rescue are mainly based on helicopter and search and rescue ship, but helicopter is to be difficult to smooth flight in inclement weather, pilot to be considered and the safety factors of rescue worker self, so wasting substantial amounts of rescue time sometimes, and search and rescue ship because of low visibility, also it is difficult to reach the effect of Quick rescue, this often makes rescue worker lose gold rescue time, add the hazardness of accident.For this it is proposed that a kind of four-axle aircraft for maritime search and rescue.
Utility model content
The purpose of this utility model is to provide a kind of four-axle aircraft for maritime search and rescue, with the problem solving to propose in above-mentioned background technology.
For achieving the above object, this utility model following technical scheme of offer: a kind of four-axle aircraft for maritime search and rescue, including aircraft frame and chassis, corner, described aircraft frame surface is equipped with propeller mount, described propeller mount top connects propeller, it is provided with protective cover bottom described aircraft frame, described protective cover is connected to chassis, described chassis surface is provided with support shaft, described support shaft top is provided with data processor, described protective cover inner chamber is provided with searchlight, described support shaft side is provided with camera head, described camera head surface is provided with infrared probe, described center chassis point is provided with connecting shaft, described connecting shaft one end is provided with support adjusting device, described support adjusting device is rotationally connected support bar, described support bar end is provided with position-limited rack, it is provided with lifebuoy between described support bar and described position-limited rack.
Preferably, described support bar is a kind of rotary support bar, and rotational angle is 0 °-90 °.
Preferably, the length of described position-limited rack is less than the radius of described lifebuoy inner ring.
Preferably, the length of described support bar is more than the diameter of described lifebuoy outer ring.
Preferably, described data processor is a kind of data processor that can process image data, thermal imaging data and transmit signal.
nullCompared with prior art，The beneficial effects of the utility model are: the four-axle aircraft diverse in function of this kind of maritime search and rescue，Pass through camera head，This aircraft has shooting and aerial photography function，The situation on sea can be shot clearly，Pass through infrared probe，The thermal imaging picture on sea level can be obtained，Survivor can be more quickly found by thermal imaging，Data processor can the very first time by these picture transfer to rescue worker，It is easy to search and rescue person and quickly grasps the firsthand information，Simultaneously，This aircraft self hangs a lifebuoy，If survivor looked for by aircraft，Rescue worker can control bracket controller，Lifebuoy is put down，So that survivor can adhere to rescue worker arriving in now，Owing to this aircraft is unmanned，So the most there is not the safety problem of rescue personnel，More aircraft can also sent with a piece of marine site，Search efficiency can be improved.
Accompanying drawing explanation
Fig. 1 is the new overall structure schematic diagram of this practicality；
Fig. 2 is the structural representation that region placed by this practicality lifebuoy；
Fig. 3 is this utility model lifebuoy supporting bar structure schematic diagram when putting down.
In figure: 1, lifebuoy, 2, protective cover, 3, support shaft, 4, propeller mount, 5, propeller, 6, data processor, 7, aircraft frame, 8, searchlight, 9, infrared probe, 10, camera head, 11, chassis, 12, position-limited rack, 13, support bar, 14, connecting shaft, 15, support adjusting device.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole embodiments.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.
nullRefer to Fig. 1-3，A kind of technical scheme of this utility model offer: a kind of four-axle aircraft for maritime search and rescue，Including aircraft frame 7 and chassis 11，Corner, aircraft frame 7 surface is equipped with propeller mount 4，Propeller mount 4 top connects propeller 5，Protective cover 2 it is provided with bottom aircraft frame 7，Protective cover 2 is connected to chassis 11，Surface, chassis 11 is provided with support shaft 3，Support shaft 3 top is provided with data processor 6，Protective cover 2 inner chamber is provided with searchlight 8，Support shaft 3 side is provided with camera head 10，Camera head 10 surface is provided with infrared probe 9，Chassis 11 central point is provided with connecting shaft 14，Connecting shaft 14 one end is provided with support adjusting device 15，Support adjusting device 15 is rotationally connected support bar 13，Support bar 13 end is provided with position-limited rack 12，Lifebuoy 1 it is provided with between support bar 13 and position-limited rack 12.
Support bar 13 is a kind of rotary support bar 13, rotational angle is the four-axle aircraft of 0 °-90 °, the length of position-limited rack 12 is less than the four-axle aircraft of the radius of lifebuoy 1 inner ring, the length of support bar 13 is more than the diameter of lifebuoy 1 outer ring, and data processor 6 is a kind of data processor 6 that can process image data, thermal imaging data and transmit signal.
During use, this aircraft is matched with remote controller, by remote controller, data processor 6 is assigned instruction, control the course of aircraft, the speed of a ship or plane and height, the pictorial information obtained by camera head 10 and infrared probe 9 is transferred to rescue personnel by data processor 6, when aircraft finds survivor, by support adjusting device, control support bar 13, it is made to draw in, putting down lifebuoy 1, win the time of existence for survivor, support is reached the spot to rescue personnel.
Embodiment the most of the present utility model, for the ordinary skill in the art, being appreciated that in the case of without departing from principle of the present utility model and spirit and these embodiments can carry out multiple change, revise, replace and modification, scope of the present utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
- null1. the four-axle aircraft for maritime search and rescue，Including aircraft frame (7) and chassis (11)，It is characterized in that: described aircraft frame (7) corner, surface is equipped with propeller mount (4)，Described propeller mount (4) top connects propeller (5)，Described aircraft frame (7) bottom is provided with protective cover (2)，Described protective cover (2) is connected to chassis (11)，Described chassis (11) surface is provided with support shaft (3)，Described support shaft (3) top is provided with data processor (6)，Described protective cover (2) inner chamber is provided with searchlight (8)，Described support shaft (3) side is provided with camera head (10)，Described camera head (10) surface is provided with infrared probe (9)，Described chassis (11) central point is provided with connecting shaft (14)，Described connecting shaft (14) one end is provided with support adjusting device (15)，Described support adjusting device (15) is rotationally connected support bar (13)，Described support bar (13) end is provided with position-limited rack (12)，Lifebuoy (1) it is provided with between described support bar (13) and described position-limited rack (12).
- A kind of four-axle aircraft for maritime search and rescue the most according to claim 1, it is characterised in that: described support bar (13) is a kind of rotary support bar (13), and rotational angle is 0 °-90 °.
- A kind of four-axle aircraft for maritime search and rescue the most according to claim 1, it is characterised in that: the length of described position-limited rack (12) is less than the radius of described lifebuoy (1) inner ring.
- A kind of four-axle aircraft for maritime search and rescue the most according to claim 1, it is characterised in that: the length of described support bar (13) is more than the diameter of described lifebuoy (1) outer ring.
- A kind of four-axle aircraft for maritime search and rescue the most according to claim 1, it is characterised in that: described data processor (6) is a kind of data processor (6) that can process image data, thermal imaging data and transmit signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620350718.8U CN205554593U (en) | 2016-04-25 | 2016-04-25 | A four shaft air vehicle for maritime search and rescue |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620350718.8U CN205554593U (en) | 2016-04-25 | 2016-04-25 | A four shaft air vehicle for maritime search and rescue |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205554593U true CN205554593U (en) | 2016-09-07 |
Family
ID=56807296
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620350718.8U Expired - Fee Related CN205554593U (en) | 2016-04-25 | 2016-04-25 | A four shaft air vehicle for maritime search and rescue |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205554593U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107878707A (en) * | 2017-03-24 | 2018-04-06 | 吴叔枚 | A kind of water life-saving equipment |
| CN108945345A (en) * | 2017-05-11 | 2018-12-07 | 郑健 | A kind of water life-saving equipment |
| CN109110119A (en) * | 2018-08-17 | 2019-01-01 | 陕西科技大学 | A kind of waters flight deliverance apparatus |
-
2016
- 2016-04-25 CN CN201620350718.8U patent/CN205554593U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107878707A (en) * | 2017-03-24 | 2018-04-06 | 吴叔枚 | A kind of water life-saving equipment |
| CN107878707B (en) * | 2017-03-24 | 2019-10-18 | 泉州市宕存工业设计有限公司 | A kind of water life-saving equipment |
| CN108945345A (en) * | 2017-05-11 | 2018-12-07 | 郑健 | A kind of water life-saving equipment |
| CN108945345B (en) * | 2017-05-11 | 2020-08-04 | 嘉兴市荣盛救生设备有限公司 | Water rescue equipment |
| CN109110119A (en) * | 2018-08-17 | 2019-01-01 | 陕西科技大学 | A kind of waters flight deliverance apparatus |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104494821B (en) | The many rotor wing unmanned aerial vehicles of a kind of multifunction emergency rescue | |
| JP2019201409A (en) | Flight unit and control method of flight unit | |
| CN205554593U (en) | A four shaft air vehicle for maritime search and rescue | |
| CN205661673U (en) | 360 degrees carry mechanisms that take photo by plane of unmanned aerial vehicle | |
| CN104483987B (en) | Unmanned plane is left a blank monitoring system | |
| CN106114881B (en) | Unmanned plane | |
| CN207173966U (en) | Hovering and flight instruments |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160907 Termination date: 20170425 |